发明名称 |
VARIABLE FAN INLET GUIDE VANE ASSEMBLY, TURBINE ENGINE WITH SUCH AN ASSEMBLY AND CORRESPONDING CONTROLLING METHOD |
摘要 |
A turbine engine includes a plurality of variable fan inlet guide vanes. Where the turbine engine is a tip turbine engine, the variable fan inlet guide vanes permit the ability to control engine stability even though the fan-turbine rotor assembly is directly coupled to the axial compressor at a fixed rate. The fan inlet guide vanes may be actuated from an inner diameter of the fan inlet guide vanes.
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申请公布号 |
US2009074568(A1) |
申请公布日期 |
2009.03.19 |
申请号 |
US20040719143 |
申请日期 |
2004.12.01 |
申请人 |
SUCIU GABRIEL L;MERRY BRIAN;NORRIS JAMES W;SIRICA STEVEN J |
发明人 |
SUCIU GABRIEL L.;MERRY BRIAN;NORRIS JAMES W.;SIRICA STEVEN J. |
分类号 |
F01D17/16;F02C3/073;F02K3/068 |
主分类号 |
F01D17/16 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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